CN108646223A - A kind of civil aviation synoptic weather observation and HERALD equipment - Google Patents

A kind of civil aviation synoptic weather observation and HERALD equipment Download PDF

Info

Publication number
CN108646223A
CN108646223A CN201810598342.6A CN201810598342A CN108646223A CN 108646223 A CN108646223 A CN 108646223A CN 201810598342 A CN201810598342 A CN 201810598342A CN 108646223 A CN108646223 A CN 108646223A
Authority
CN
China
Prior art keywords
cavity
drive
rod
drive cavity
motor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
CN201810598342.6A
Other languages
Chinese (zh)
Inventor
韩磊
Original Assignee
韩磊
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 韩磊 filed Critical 韩磊
Priority to CN201810598342.6A priority Critical patent/CN108646223A/en
Publication of CN108646223A publication Critical patent/CN108646223A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/03Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver
    • G01S7/032Constructional details for solid-state radar subsystems

Abstract

The invention discloses a kind of civil aviation synoptic weather observation and HERALD equipments, including fuselage, it is arranged in the first drive cavity the first upward cavity of the fuselage inner opening and be arranged in the fuselage below first cavity, the second cavity of opening upwards is provided in the first drive cavity roof, the first rotating turret extended up and down is rotatably provided between first cavity and first drive cavity, first rotating turret outer surface in first cavity, which can slide up and down, is provided with sliding sleeve, sliding eye is equipped in the sliding sleeve, annular chamber is equipped in the sliding eye inner wall;The configuration of the present invention is simple; it is easy to operate; drive powershift is synchronous with door unlatching to carry out by using the same power source; steering mechanism is set during operation again; it cooperates and does not influence between each process; reach storage protection weather radar purpose, while realizing that radar turns to swing function, improves equipment practicability.

Description

A kind of civil aviation synoptic weather observation and HERALD equipment
Technical field
The present invention relates to meteorological field, specifically a kind of civil aviation synoptic weather observation and HERALD equipment.
Background technology
With the development of science and technology, social progress, country promotes always high-tech development, in meteorological field, always There are a relatively difficult technical problem, it is exactly that common weather radar movement is inconvenient, and can not be stored in bad weather, makes At the accelerated ageing and damage of weather radar, this device efficiently solves the problems, such as this.
Invention content
Technical problem to be solved by the invention is to provide a kind of civil aviation synoptic weather observation and HERALD equipments, can solve The problems in certainly above-mentioned present technology.
The present invention is achieved through the following technical solutions:A kind of civil aviation synoptic weather observation and forecast of the present invention is set It is standby, including fuselage, be arranged and be located at described the in the first upward cavity of the fuselage inner opening and being arranged in the fuselage The first drive cavity below one cavity, is provided with the second cavity of opening upwards in the first drive cavity roof, and described first The first rotating turret extended up and down, the institute in first cavity are rotatably provided between cavity and first drive cavity It states the first rotating turret outer surface and can slide up and down and be provided with sliding sleeve, sliding eye, the sliding eye are equipped in the sliding sleeve It is equipped with annular chamber in inner wall, is hingedly connected with the head rod upwardly extended on the left of the sliding sleeve, in first drive cavity First rotating turret outer surface be installed with first bevel gear, up and down perforative first is equipped in first rotating turret Threaded hole, the first threaded hole screw-internal thread fit are connected with the first screw thread extended up and down, in the first threaded rod bottom wall Equipped with the rectangular cavity that Open Side Down, the square pole extended downwardly, the square pole bottom are slidably provided in the rectangular cavity Portion is fixedly connected with the second cavity bottom wall, and third cavity, third cavity bottom are equipped in the first threaded rod roof It is fixedly installed first motor in wall, the third cavity roof is extended through on the first motor driving axial and stretches out outside Space and end are fixedly connected with rotation seat, and opening upwards and the 4th cavity of left and right perforation, institute are provided in the rotation seat It states and is hingedly connected with the second connecting rod upwardly extended between end wall before and after the 4th cavity, second connecting rod upwardly extends top Portion end is fixedly connected with radome, and the radome bottom left is articulated and connected with the head rod, and described first passes The 5th cavity is provided with and communicated on rear side of dynamic chamber in end wall, the second drive cavity of opening upwards is equipped in the 5th cavity bottom wall, It is provided with and communicated with the third drive cavity upwardly extended in end wall on rear side of 5th cavity, can be slided up and down in the 5th cavity Be provided with the first sliding shoe, the second threaded hole up and down, second threaded hole are provided in first sliding shoe Screw-internal thread fit is connected with the second threaded rod extended up and down, and the second threaded rod bottom end is rotatably dispose in the described 5th In cavity bottom wall, the second threaded rod top end and the second motor power being fixedly installed in the 5th cavity roof Connection, the second screw thread rod outer surface are installed with second bevel gear, fix and set in the end wall of the first sliding shoe front side It is equipped with third motor, extending end is installed with and the first bevel gear disengaging cooperation third motor driving shaft forward Third hand tap gear, first turn of end wall before and after second drive cavity is rotatably provided through in second drive cavity Axis, the first rotating shaft outer surface in second drive cavity are installed with the 4th cone engaged with the third hand tap gear Gear, the third drive cavity rear side end wall is interior to be equipped with the 4th drive cavity upwardly extended, and the third drive cavity and the 4th pass Front and back the second shaft extended is rotatably provided between dynamic chamber, second shaft front side end in the third drive cavity It holds and is installed with the 5th bevel gear engaged with the second bevel gear, outside second shaft in the 4th drive cavity Surface is installed with first pulley, and front and back extension is rotatably provided between the 4th drive cavity and first cavity Third shaft, the third shaft outer surface in the 4th drive cavity is installed with the second belt wheel, the first band It is connected by belt transmission between wheel and second belt wheel, the third shaft front side end in first cavity is solid Dingan County is equipped with third connecting rod.
Preferably technical solution, the fuselage roof are provided with door, opening are provided in the door lower face The 6th downward cavity, what can be horizontally slipped in the 6th cavity is provided with the second sliding shoe, is set in the second sliding shoe It is equipped with the perforative unthreaded hole in left and right, the polished rod that left and right extends, polished rod left and right sides end are slidably connected in the unthreaded hole End is fixedly installed in the 6th cavity left hand end wall, the second sliding shoe bottom and the first cavity left end wall top Articulated connection, the third connecting rod top are articulated and connected with end wall on rear side of the 6th cavity.
Preferably technical solution, the radome top are provided with signal receiver, the signal receiver and institute It states and is fixedly connected with fixed link between radome.
Preferably technical solution, the first rotating shaft left and right ends are fixedly installed wheel.
Preferably technical solution, the guide runner being provided in the first threaded hole left hand end wall outside connection, institute State can horizontally slip in guide runner be provided with third sliding shoe, the guide runner is provided with the inside limit that is open in end wall up and down Position slot, is slidably fitted with the limited block being fixedly connected with the third sliding shoe in the limiting slot, on the limit trough end wall It is installed with the top pressure spring to offset with the limited block, appearance is provided with the first inclined-plane, institute in the middle part of first threaded rod It states third sliding shoe and is equipped with the second inclined-plane coordinated with first inclined-plane close to first threaded rod side.
The beneficial effects of the invention are as follows:The present invention equipment in the initial state, the first motor, the second motor and Third motor is in stationary state, and first sliding shoe is located at the 5th cavity bottom, the triconodont Wheel is engaged with the 4th bevel gear, and the third hand tap gear is detached from the first bevel gear.
Described in the equipment of the present invention, in use, starting the third motor first, the third motor rotation drives Third hand tap gear rotates, and the third hand tap gear rotation drives the 4th bevel gear rotation, the 4th bevel gear to rotate band The dynamic first rotating shaft rotation, the first rotating shaft rotation drive the vehicle wheel rotation, the vehicle wheel rotation to move the equipment To suitable area, the third motor stops, and starts second motor, and the second motor rotation drives second screw thread Bar rotates, and second threaded rod rotation drives first sliding shoe to move up, and first sliding shoe, which moves up, drives described the Third hand tap gear moves up, and when the third hand tap gear is engaged with the first bevel gear, stops second motor, at the same time The second threaded rod rotation drives the second bevel gear rotation, the second bevel gear rotation to drive the 5th bevel gear Rotation, the 5th bevel gear rotation drive the first pulley rotation, the first pulley to drive the second belt wheel rotation, The second belt wheel rotation drives the third connecting rod rotation, the third connecting rod to drive the door rotation, the storehouse Door rotation is slided with polished rod described in time delay, and when second motor stops, the door is just flat with end wall on the left of the fuselage Row, the door opening, starts the third motor rotation at this time, and the third motor rotation drives the third hand tap gear to turn Dynamic, the third hand tap gear rotation drives the first bevel gear rotation, the first bevel gear rotation to drive described first turn Moving frame rotation, the first rotating turret rotation drive first threaded rod to rise, and first threaded rod rises described in drive Radome rises, and the radome, which rises, drives the head rod to rise, and the head rod, which rises, drives the cunning Set moves up, described in the dislocation on the slip guiding sleeve when the first rotating turret top end, first inclined-plane and second inclined-plane It abuts, second inclined-plane moves to the annular chamber in the second ramp effect bottom left, the sliding sleeve is locked, described at this time Radome
It is pushed out outside the equipment, first threaded rod continues to move up, and the radome is pushed to turn left, when going to Third motor stalls described in proper angle, start the first motor rotation at this time, and the first motor rotation drives institute Radome is stated to circumferentially rotate, when the signal receiver receive signal it is effective when stop the first motor.
When the equipment is completed in use, third motor described in reverse starting, the radome will be incorporated into described first Then cavity stops the third motor, start second motor and rotate backward, the third hand tap gear is bored with the described 4th Gear engages, while the door is closed, and the equipment restPoses.
The configuration of the present invention is simple, it is easy to operate, drive powershift synchronous with door unlatching by using the same power source It carries out, and steering mechanism is set during operation, cooperate between each process and do not influence, reach storage protection Weather radar purpose, while realizing that radar turns to swing function, improve equipment practicability.
Description of the drawings
The present invention is described in detail by following specific embodiment and attached drawing for ease of explanation,.
Fig. 1 is a kind of civil aviation synoptic weather observation and the HERALD equipment overall structure diagram of the present invention;
Fig. 2 is the structural schematic diagram of A in Fig. 1;
Fig. 3 is the structural schematic diagram of B-B in Fig. 1.
Specific implementation mode
As shown in Figure 1-Figure 3, a kind of civil aviation synoptic weather observation of the invention and HERALD equipment, including fuselage 100, setting It is located at first cavity in the fuselage 100 in the first upward cavity 101 of 100 inner opening of the fuselage and setting First drive cavity 113 of 101 lower sections, the second cavity 115 of opening upwards, institute are provided in 113 roof of the first drive cavity State the first rotating turret 131 for being rotatably provided between the first cavity 101 and first drive cavity 113 and extending up and down, institute It states 131 outer surface of the first rotating turret in the first cavity 101 and can slide up and down and be provided with sliding sleeve 110, the sliding sleeve 110 It is interior to be equipped with sliding eye 112, annular chamber 111,110 left side articulated connection of the sliding sleeve are equipped in 112 inner wall of the sliding eye There is the head rod 104 upwardly extended, peace is fixed in 131 outer surface of the first rotating turret in first drive cavity 113 Upper and lower perforative first threaded hole 118, first screw thread are equipped with equipped with first bevel gear 114, in first rotating turret 131 118 screw-internal thread fit of hole is connected with the first screw thread 119 extended up and down, be equipped in 119 bottom wall of the first threaded rod opening to Under rectangular cavity 109, be slidably provided with the square pole 108 extended downwardly, the square pole 108 in the rectangular cavity 109 Bottom is fixedly connected with 115 bottom wall of the second cavity, and third cavity 106 is equipped in 119 roof of the first threaded rod, described It is fixedly installed first motor 107 in 106 bottom wall of third cavity, is extended through on 107 driving axial of the first motor described 106 roof of third cavity stretches out exterior space and end is fixedly connected with rotation seat 120, is provided with out in the rotation seat 120 Mouthful upwards and the 4th cavity 105 of left and right perforation, it is hingedly connected with before and after the 4th cavity 105 and to upwardly extend between end wall Second connecting rod 137, second connecting rod 137 upwardly extend top end and are fixedly connected with radome 102, the radome 102 bottom lefts are articulated and connected with the head rod 104, are provided with and communicated in first drive cavity, 113 rear side end wall 5th cavity 143, interior the second drive cavity 139 for being equipped with opening upwards of 143 bottom wall of the 5th cavity, the 5th cavity 143 The third drive cavity 153 upwardly extended is provided with and communicated in rear side end wall, can slide up and down setting in the 5th cavity 143 There is the first sliding shoe 147, the second threaded hole 145 up and down, second screw thread are provided in first sliding shoe 147 145 screw-internal thread fit of hole is connected with the second threaded rod 142 extended up and down, and 142 bottom end of the second threaded rod rotation is set It is placed in 143 bottom wall of the 5th cavity, 142 top end of the second threaded rod and is fixedly installed on the 5th cavity 152 be connected by power of the second motor in 143 roofs, 142 outer surface of the second threaded rod are installed with second bevel gear 148, third motor 146,146 driving axial of third motor are fixedly installed in first sliding shoe, 147 front side end wall Preceding extending end is installed with the third hand tap gear 144 that cooperation is detached from the first bevel gear 114, second drive cavity The first rotating shaft 140 of end wall before and after second drive cavity 139, second drive cavity are rotatably provided through in 139 140 outer surface of the first rotating shaft in 139 is installed with the 4th bevel gear 138 engaged with the third hand tap gear 144, It is equipped with the 4th drive cavity 155 upwardly extended in 153 rear side end wall of the third drive cavity, the third drive cavity 153 and the Front and back the second shaft 149 extended is rotatably provided between four drive cavities 155, it is described in the third drive cavity 153 Second shaft, 149 front side end is installed with the 5th bevel gear 151 engaged with the second bevel gear 148, and the described 4th 149 outer surface of the second shaft in drive cavity 155 is installed with first pulley 150, the 4th drive cavity 155 and institute It states and is rotatably provided with the front and back third shaft 157 extended between the first cavity 101, the institute in the 4th drive cavity 155 It states 157 outer surface of third shaft and is installed with the second belt wheel 156, between the first pulley 150 and second belt wheel 156 It is driven and is connected by belt 155,157 front side end of third shaft in first cavity 101 is installed with the Three connecting rods 123.
Valuably, the top of the fuselage 100 is provided with door 124, is provided with that Open Side Down in 124 lower face of the door The 6th cavity 127, what can be horizontally slipped in the 6th cavity 127 is provided with the second sliding shoe 125, the second sliding shoe It is provided with the perforative unthreaded hole 128 in left and right in 125, the polished rod 126 that left and right extends, institute are slidably connected in the unthreaded hole 128 It states 126 left and right sides end of polished rod to be fixedly installed in 127 left hand end wall of the 6th cavity, 125 bottom of the second sliding shoe It is articulated and connected at the top of portion and first cavity, 101 left end wall, 123 top of the third connecting rod and the 6th cavity 127 Rear side end wall is articulated and connected, convenient for protecting the equipment.
Valuably, 102 top of the radome is provided with signal receiver 122, the signal receiver 122 and the thunder Up to fixed link 121 is fixedly connected between cover 102, receive satellite-signal convenient for the equipment.
Valuably, 140 left and right ends of the first rotating shaft are fixedly installed wheel 141, are moved convenient for the equipment.
Valuably, the guide runner 135 being provided in 118 left hand end wall of the first threaded hole outside connection, the slide guide What can be horizontally slipped in slot 135 is provided with third sliding shoe 136, and it is inside that opening is provided in about 135 end wall of the guide runner Limiting slot 133, be slidably fitted with the limited block 130 being fixedly connected with the third sliding shoe 136 in the limiting slot 133, The top pressure spring 134 to offset with the limited block 130 is installed on 133 end wall of the limiting slot, convenient for fastening the cunning Set 110, first threaded rod, 119 middle part appearance are provided with the first inclined-plane 117, and the third sliding shoe 136 is close to described the One threaded rod, 119 side is equipped with the second inclined-plane 129 coordinated with first inclined-plane 117.
In the initial state, the first motor 107, the second motor 152 and third motor 146 are equal for the equipment of the present invention It remains static, first sliding shoe 147 is located at 143 bottom of the 5th cavity, the third hand tap gear 144 It is engaged with the 4th bevel gear 138, the third hand tap gear 144 is detached from the first bevel gear 114.
When with the equipment of the present invention, in use, starting the third motor 146 first, the third motor 146 rotates band The dynamic third hand tap gear 144 rotates, and the rotation of the third hand tap gear 144 drives the 4th bevel gear 138 rotation, and described the The rotation of four bevel gears 138 drives the first rotating shaft 140 to rotate, and the rotation of the first rotating shaft 140 drives 141 turns of the wheel Dynamic, to suitable area, the third motor 146 stops the mobile equipment of the rotation of the wheel 141, starts second motor 152, the rotation of the second motor 152 drives second threaded rod 142 to rotate, and the rotation of the second threaded rod 142 drives institute It states the first sliding shoe 147 to move up, first sliding shoe 147, which moves up, drives the third hand tap gear 144 to move up, when the third When bevel gear 144 engages with the first bevel gear 114, stop second motor 146, at the same time second threaded rod 142 rotations drive the second bevel gear 148 to rotate, and the rotation of the second bevel gear 148 drives 151 turns of the 5th bevel gear Dynamic, the 5th bevel gear 151 rotation drives the first pulley 150 to rotate, and the first pulley 150 drives second band 156 rotation of wheel, the rotation of the second belt wheel 156 drive the third connecting rod 123 to rotate, and the third connecting rod 123 drives The door 124 rotates, and the rotation of the door 124 is slided with polished rod described in time delay 126, when second motor 146 stops The door 124 is just parallel with 100 left side end wall of the fuselage, and the door is opened at this time, starts the third motor 146 Rotation, the rotation of third motor 146 drive the third hand tap gear 144 to rotate, and the rotation of the third hand tap gear 144 drives institute The rotation of first bevel gear 114 is stated, the rotation of the first bevel gear 114 drives first rotating turret 131 to rotate, described first turn The rotation of moving frame 131 drives first threaded rod 119 to rise, and first threaded rod 119, which rises, to be driven on the radome 102 It rises, the radome 102, which rises, drives the head rod 104 to rise, and the head rod 104, which rises, drives the cunning Set 110 moves up, described in the dislocation on the slip guiding sleeve 110 when the first 131 top end of rotating turret, first inclined-plane 117 with Second inclined-plane 129 abuts, and second inclined-plane 129 moves to the annular chamber in second inclined-plane 129 effect bottom left 111, the sliding sleeve 110 is locked, at this time the radome 102
It being pushed out outside the equipment, first threaded rod 119 continues to move up, and the radome 102 is pushed to turn left, It stops operating when going to third motor 146 described in proper angle, starts the rotation of the first motor 107, first electricity at this time The rotation of machine 107 drives the radome 102 to circumferentially rotate, when the signal receiver 122 receive signal it is effective when stop institute State first motor 107.
When the equipment is completed in use, third motor 146 described in reverse starting, the radome 102 will be incorporated into institute The first cavity 101 is stated, the third motor 146 is then stopped, starting second motor 152 and rotates backward, the third cone Gear 144 is engaged with the 4th bevel gear 138, while the door is closed, and the equipment restPoses.
The beneficial effects of the invention are as follows:The present invention equipment in the initial state, the first motor, the second motor and Third motor is in stationary state, and first sliding shoe is located at the 5th cavity bottom, the triconodont Wheel is engaged with the 4th bevel gear, and the third hand tap gear is detached from the first bevel gear.
Described in the equipment of the present invention, in use, starting the third motor first, the third motor rotation drives Third hand tap gear rotates, and the third hand tap gear rotation drives the 4th bevel gear rotation, the 4th bevel gear to rotate band The dynamic first rotating shaft rotation, the first rotating shaft rotation drive the vehicle wheel rotation, the vehicle wheel rotation to move the equipment To suitable area, the third motor stops, and starts second motor, and the second motor rotation drives second screw thread Bar rotates, and second threaded rod rotation drives first sliding shoe to move up, and first sliding shoe, which moves up, drives described the Third hand tap gear moves up, and when the third hand tap gear is engaged with the first bevel gear, stops second motor, at the same time The second threaded rod rotation drives the second bevel gear rotation, the second bevel gear rotation to drive the 5th bevel gear Rotation, the 5th bevel gear rotation drive the first pulley rotation, the first pulley to drive the second belt wheel rotation, The second belt wheel rotation drives the third connecting rod rotation, the third connecting rod to drive the door rotation, the storehouse Door rotation is slided with polished rod described in time delay, and when second motor stops, the door is just flat with end wall on the left of the fuselage Row, the door opening, starts the third motor rotation at this time, and the third motor rotation drives the third hand tap gear to turn Dynamic, the third hand tap gear rotation drives the first bevel gear rotation, the first bevel gear rotation to drive described first turn Moving frame rotation, the first rotating turret rotation drive first threaded rod to rise, and first threaded rod rises described in drive Radome rises, and the radome, which rises, drives the head rod to rise, and the head rod, which rises, drives the cunning Set moves up, described in the dislocation on the slip guiding sleeve when the first rotating turret top end, first inclined-plane and second inclined-plane It abuts, second inclined-plane moves to the annular chamber in the second ramp effect bottom left, the sliding sleeve is locked, described at this time Radome
It is pushed out outside the equipment, first threaded rod continues to move up, and the radome is pushed to turn left, when going to Third motor stalls described in proper angle, start the first motor rotation at this time, and the first motor rotation drives institute Radome is stated to circumferentially rotate, when the signal receiver receive signal it is effective when stop the first motor.
When the equipment is completed in use, third motor described in reverse starting, the radome will be incorporated into described first Then cavity stops the third motor, start second motor and rotate backward, the third hand tap gear is bored with the described 4th Gear engages, while the door is closed, and the equipment restPoses.
The configuration of the present invention is simple, it is easy to operate, drive powershift synchronous with door unlatching by using the same power source It carries out, and steering mechanism is set during operation, cooperate between each process and do not influence, reach storage protection Weather radar purpose, while realizing that radar turns to swing function, improve equipment practicability.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any The change or replacement expected without creative work, should be covered by the protection scope of the present invention.Therefore, of the invention Protection domain should be determined by the scope of protection defined in the claims.

Claims (5)

1. a kind of civil aviation synoptic weather observation and the HERALD equipment of the present invention, including fuselage, setting the fuselage inner opening to On the first cavity and the first drive cavity for being arranged in the fuselage below first cavity, it is characterised in that: The second cavity of opening upwards is provided in the first drive cavity roof, between first cavity and first drive cavity It rotatably is provided with the first rotating turret extended up and down, first rotating turret outer surface in first cavity can be upper and lower Sliding is provided with sliding sleeve, and sliding eye is equipped in the sliding sleeve, annular chamber, the sliding sleeve are equipped in the sliding eye inner wall Left side is hingedly connected with the head rod upwardly extended, and first rotating turret outer surface in first drive cavity is fixed First bevel gear is installed, is equipped with upper and lower perforative first threaded hole in first rotating turret, spiral shell in first threaded hole Line is connected with the first screw thread extended up and down, and the rectangular cavity that Open Side Down is equipped in the first threaded rod bottom wall, described The square pole extended downwardly is slidably provided in rectangular cavity, the square pole bottom is fixed with the second cavity bottom wall to be connected It connects, third cavity is equipped in the first threaded rod roof, first motor is fixedly installed in the third cavity bottom wall, it is described The third cavity roof stretching exterior space is extended through on first motor driving axial and end is fixedly connected with rotation seat, It is provided with opening upwards in the rotation seat and controls the 4th cavity of perforation, hingedly connects between end wall before and after the 4th cavity It is connected to the second connecting rod upwardly extended, second connecting rod upwardly extends top end and is fixedly connected with radome, described Radome bottom left is articulated and connected with the head rod, and the 5th is provided with and communicated in end wall on rear side of first drive cavity Cavity, interior the second drive cavity for being equipped with opening upwards of the 5th cavity bottom wall, the interior connection of the 5th cavity rear side end wall are set It is equipped with the third drive cavity upwardly extended, can slide up and down in the 5th cavity and be provided with the first sliding shoe, described first The second threaded hole up and down is provided in sliding shoe, the second threaded hole screw-internal thread fit is connected with extended up and down Two threaded rods, the second threaded rod bottom end are rotatably dispose in the 5th cavity bottom wall, second threaded rod top Portion end is connect with the second motor power being fixedly installed in the 5th cavity roof, and the second screw thread rod outer surface is solid Dingan County is equipped with second bevel gear, is fixedly installed third motor in the end wall of the first sliding shoe front side, the third motor drives Extending end is installed with the third hand tap gear that cooperation is detached from the first bevel gear, second drive cavity to moving axis forward Inside rotatably it is provided through the first rotating shaft of end wall before and after second drive cavity, described in second drive cavity One shaft outer surface is installed with the 4th bevel gear engaged with the third hand tap gear, the third drive cavity rear side end wall It is interior equipped with the 4th drive cavity upwardly extended, front and back prolong rotatably is provided between the third drive cavity and the 4th drive cavity The second shaft stretched, the second shaft front side end in the third drive cavity are installed with and the second bevel gear 5th bevel gear of engagement, second shaft outer surface in the 4th drive cavity is installed with first pulley, described The front and back third shaft extended is rotatably provided between 4th drive cavity and first cavity, in the 4th drive cavity Third shaft outer surface be installed with the second belt wheel, passed by belt between the first pulley and second belt wheel Dynamic to be connected, the third shaft front side end in first cavity is installed with third connecting rod.
2. a kind of civil aviation synoptic weather observation according to claim 1 and HERALD equipment, it is characterised in that:The fuselage top Portion is provided with door, and the 6th cavity that Open Side Down is provided in the door lower face, cunning can be controlled in the 6th cavity Dynamic is provided with the second sliding shoe, and the perforative unthreaded hole in left and right is provided in the second sliding shoe, is slidably matched in the unthreaded hole It is connected with the polished rod that left and right extends, end is fixedly installed in the 6th cavity left hand end wall at left and right sides of the polished rod, institute It states the second sliding shoe bottom to be articulated and connected at the top of the first cavity left end wall, the third connecting rod top and the described 6th End wall articulated connection on rear side of cavity.
3. a kind of civil aviation synoptic weather observation according to claim 1 and HERALD equipment, it is characterised in that:The radome Top is provided with signal receiver, and fixed link is fixedly connected between the signal receiver and the radome.
4. a kind of civil aviation synoptic weather observation according to claim 1 and HERALD equipment, it is characterised in that:Described first turn Axis left and right ends are fixedly installed wheel.
5. a kind of civil aviation synoptic weather observation according to claim 1 and HERALD equipment, it is characterised in that:First spiral shell The external guide runner of connection is provided in pit left hand end wall, the third that is provided with that can be horizontally slipped in the guide runner is slided Block, the guide runner are provided with the inside limiting slot that is open in end wall up and down, are slidably fitted in the limiting slot and described the The limited block that three sliding shoes are fixedly connected is installed with the top pressure bullet to offset with the limited block on the limit trough end wall Spring, the first threaded rod middle part appearance are provided with the first inclined-plane, and the third sliding shoe is close to first threaded rod side Equipped with the second inclined-plane coordinated with first inclined-plane.
CN201810598342.6A 2018-06-12 2018-06-12 A kind of civil aviation synoptic weather observation and HERALD equipment Withdrawn CN108646223A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810598342.6A CN108646223A (en) 2018-06-12 2018-06-12 A kind of civil aviation synoptic weather observation and HERALD equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810598342.6A CN108646223A (en) 2018-06-12 2018-06-12 A kind of civil aviation synoptic weather observation and HERALD equipment

Publications (1)

Publication Number Publication Date
CN108646223A true CN108646223A (en) 2018-10-12

Family

ID=63752415

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810598342.6A Withdrawn CN108646223A (en) 2018-06-12 2018-06-12 A kind of civil aviation synoptic weather observation and HERALD equipment

Country Status (1)

Country Link
CN (1) CN108646223A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110806583A (en) * 2019-11-21 2020-02-18 武义仙合电子有限公司 Small-size weather radar device that can accomodate

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110806583A (en) * 2019-11-21 2020-02-18 武义仙合电子有限公司 Small-size weather radar device that can accomodate

Similar Documents

Publication Publication Date Title
CN108732644A (en) A kind of removable civil aviation synoptic weather observation and HERALD equipment
CN109818397A (en) A kind of new energy automatic charging stake
CN106906755B (en) A kind of bridge equipment
CN108646223A (en) A kind of civil aviation synoptic weather observation and HERALD equipment
CN109084493A (en) A kind of solar energy is from trend day tracking device and its application method
CN109994811A (en) A kind of sensing equipment of portable aerial radiation wave
CN107055363B (en) A kind of irrigating apparatus
CN109004519A (en) Manufacture high-conductivity atmospheric layer active lightning protection lightning protection method and device
CN109217792A (en) A kind of driving device for tuned resonant circuit
CN104862929A (en) Opening and closing device of upper cover of washing machine and washing machine
CN109067332A (en) A kind of device of solar generating
CN109163538A (en) A kind of weaving drying unit
CN109048267A (en) A kind of hinge leaf device
CN106256581A (en) Automatic antitheft automobile sun-shading cover
CN109084494A (en) A kind of solar energy is from trend day tracking device
CN108238493A (en) A kind of novel power cable device
CN109057888A (en) A kind of highly efficient cooling device of outer shell flanch of steam turbine
CN108970081A (en) A kind of beach volleyball judges' box
CN108590494A (en) A kind of multifunctional door and window
CN108354189A (en) A kind of modified agricultural and sideline product intensive processing device
CN208501285U (en) The horizontal opening structure of dye jigger
CN210617952U (en) Hydraulic control structure for agricultural three-wheel self-discharging function
CN108616037A (en) A kind of discontinuous corona discharge pulse lightning rod and its application method
CN206418691U (en) A kind of flexible awning
CN208761621U (en) A kind of stopper transmitting carrying device blocking

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
WW01 Invention patent application withdrawn after publication

Application publication date: 20181012

WW01 Invention patent application withdrawn after publication